1) hypersonic cruise missile
高超声速巡航导弹
1.
Method Research on Trajectory Design and Optimization of Hypersonic Cruise Missile;
高超声速巡航导弹弹道设计与优化方法研究
2.
Aimed at the complex dynamic course of combat engagement,a framework for hypersonic cruise missile combat engagement simulation is established.
针对攻防对抗这一复杂的动态过程,建立了高超声速巡航导弹攻防对抗仿真体系,并在此体系框架下,分别给出了作战环境模型、结果评判模型和进攻方与防御方的交战仿真模型。
3.
In the conceptual design of hypersonic cruise missiles,the evaluation of the missile combat effectiveness is necessary to avoid excessive index in the missile performance requirements.
在高超声速巡航导弹概念设计阶段,为了避免对某些性能指标要求过高,需要对其作战效能进行评估与分析。
2) supersonic cruise missile
超音速巡航导弹
3) supersonic cruise
超声速巡航
1.
The advantages of the fourth generation engine in supersonic cruise, visibility, life cycle cost (LCC) and the potential have been analyzed.
本文介绍了国外第四代战斗机对动力装置的要求,归纳了第四代战斗机发动机的主要新技术,分析了第四代战斗机发动机在超声速巡航、可探测性、全寿命费用和发展潜力等方面所具有的优势,最后总结了第四代战斗机发动机发展过程中的几个重要特点,并对发动机技术发展进行了展望。
2.
Focused on the features of stealth, super maneuverability and supersonic cruise of the future fighter, the authors identified the main difficulties and gave some practical solutions to lift drag characteristics at sub /tran sonic speed, high A.
针对未来歼击机隐身、高机动和超声速巡航的特点 ,分析了主要的设计矛盾 ,并且就亚跨声速升阻特性、低速大迎角特性和超声速阻力特性等若干设计问题提出了具体的解决方案。
4) supersonic maneuverable missile
超声速飞航导弹
1.
A prediction method of liftdrag ratio of supersonic maneuverable missile was given.
参考飞机/发动机一体化设计的思路,建立了基于能量法的超声速飞航导弹/冲压发动机一体化设计的约束分析和任务分析模型。
5) hypersonic cruise vehicle
高超声速巡航飞行器
1.
Based on system performance,guided by an object-oriented method,an integrated optimization design system of a hypersonic cruise vehicle was built through VC++.
从总体性能指标角度出发,采用面向对象的编程方法,基于Visual C++开发了高超声速巡航飞行器气动布局优化软件。
2.
An airframe/propulsion system integrated design o f hypersonic cruise vehicle overall performance analysis model is set up.
建立了高超声速巡航飞行器机身/推进系统一体化设计模型,对高超声速巡航飞行器机体/推进系统设计参数对性能的影响进行了分析,提出了一种新的设计参数灵敏度分析方法和设计参数取值域界定方法,确定了各设计参数的影响等级并对设计参数取值域进行了划分。
6) Hypersonic Missile
高超声速导弹
1.
Study on Robust Variable Structure Control for Hypersonic Missile in Reentry;
高超声速导弹再入的鲁棒变结构控制方法研究
补充资料：“战斧”巡航导弹